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Airworthiness directives › 2016-17-02

AD 2016-17-02 Airworthiness Directives; Dassault Aviation Airplanes

Superseded. This directive was replaced by AD 2017-19-17. Work to the current one.
2016-09-06
2016-08-19
39-18615
FAA-2016-8843
Airframe
2017-19-17

Models named: FALCON 900EX, FALCON 2000EX. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to the Dassault Aviation airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category. (1) Model FALCON 900EX airplanes, serial numbers (S/Ns) 270 through 291 inclusive and 294. (2) Model FALCON 2000EX airplanes, S/Ns 263 through 305 inclusive, 307 through 313 inclusive, 315, 320, and 701 through 734 inclusive.

Compliance

Comply with this AD within the compliance times specified, unless already done.

Required actions

(1) For Model FALCON 900EX airplanes on which the actions specified in Dassault Service Bulletin F900EX-464 have not been accomplished: Within 10 flight cycles after the effective date of this AD, revise Section 4-200-05A, “OPERATION IN ICING CONDITIONS,” of the Model FALCON 900EX AFM to include the information in figure 1 to paragraph (g)(1) of this AD, and thereafter operate the airplane accordingly. The AFM revision may be done by inserting a copy of this AD into the AFM. ER19AU16.004 (2) For Model FALCON 2000EX airplanes on which the actions specified in Dassault Service Bulletin F2000EX-393 have not been accomplished: Within 10 flight cycles after the effective date of this AD, revise Section 4-200-05A, “OPERATION IN ICING CONDITIONS,” of the Model FALCON 2000EX AFM to include the information in figure 2 to paragraph (g)(2) of this AD, and thereafter operate the airplane accordingly. The AFM revision may be done by inserting a copy of this AD into the AFM. ER19AU16.005

Unsafe condition

This AD was prompted by a design review of in-production airplanes that identified a deficiency in certain wing anti-ice system ducting. A deficiency in the wing anti-ice system ducting could lead to undetected, reduced performance of the wing anti-ice system, with potential ice accretion and ingestion, possibly resulting in degraded engine power and degraded handling characteristics of the airplane. We are issuing this AD to ensure the flight crew has procedures for operating an airplane in icing conditions.

Affected ADs

None.

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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1